摘要
在研究弹道导弹光学瞄准技术的基础上,提出了飞航导弹方位瞄准的新方案。推导了光学方位传递对准误差方程并进行了误差分析。经过两个型号惯导系统的对准试验,证明该方案具有一定的实用性和可靠性。
Based upon the optical orientation of tallistic missile,new azimuth orientation concept for cruise missile is presented.The error trasfer equation of optical azimuth orientation is derived and analysed.The testing results in two inertial guidance systems show that the concept is practicable and reliable.
出处
《战术导弹技术》
1994年第1期25-32,共8页
Tactical Missile Technology
关键词
飞航导弹
光学瞄准
误差分析
导弹
Cruise missile
Optical direction finding
Alignment
Error analysis
